STC SR00538SE

Supplemental type certificate · Onboard Systems International

Holder
Onboard Systems International · United States
Status
Current · Reissued
Status date
October 7, 2021
Applied
May 28, 1998
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21
Data sheet
TCDSH2SW

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Fabrication of Onboard Systems Model 200-232-00 cargo hook kit

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ SR00538SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206A and 206B Fabrication of Onboard Systems Model 200-232-00 cargo hook kit in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-039-00, dated June 26, 2000, or later FAA approved revision; and installation of this replacement cargo hook in accordance with FAA approved Onboard Systems Owner’s Manual No. 120-074-00, dated June 26, 2000, or later FAA approved revision. Inspect this cargo hook kit in accordance with Onboard Systems Service Manual No. 122-002-00, dated June 12, 2000, or later FAA approved revision.

Approval of this change in type design applies only to those Bell model rotorcraft listed above, which were previously equipped with an FAA approved installation of Bell cargo hook suspension assembly, P/N 206-706-335-1, -101, or -103; Bell cargo hook provisions kit, P/N 206 706-335-3, -5 or -105; and Breeze Eastern cargo hook P/N SP-4232-4, -5, or -5L. This approval should not be extended to rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Modified rotorcraft must be operated in accordance with an FAA approved copy of Onboard Rotorcraft Flight Manual Supplement (RFMS) No. 120-074-00, dated July 27, 1998, or later FAA approved revision.

May 28, 1998 October 7, 2021 July 27, 2000; January 13, 2003 For Acting Manager, Seattle ACO Branch 2 July 27, 1998

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ SR00538SE 2

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Bell Helicopter Textron (Canada)206AH2SW
Bell Helicopter Textron (Canada)206BH2SW

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
October 7, 2021Reissued, currentCertificate
October 7, 2021Reissued, earlier issueCertificate
January 13, 2003Amended, earlier issueCertificate